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Space tug avionics definition study. Volume 3: Avionics baseline configuration definitionThe baseline avionics systems for the space tug is comprised of a central digital computer that integrates the functions of all of the tug's subsystems by means of a redundant digital data bus. The major subsystems of the avionics system are: data management; communications; guidance, navigation, and control; rendezvous and docking; electrical power; and instrumentation. The baseline avionics system for the space tug resulting from system and subsystem trade studies is defined. Tug interfaces with the spacecraft, orbiter and the ground, and the baseline philosophy and configuration for onboard checkout of the tug are included. Baseline configurations, functional and operational features, component details and characteristics, and the supporting software are included in the subsystem descriptions.
Document ID
19750018987
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-120657
CASD-NAS-75-012-VOL-3
Report Number: NASA-CR-120657
Report Number: CASD-NAS-75-012-VOL-3
Accession Number
75N27059
Funding Number(s)
CONTRACT_GRANT: NAS8-31010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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